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57:020 Mechanics of and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 1 Chapter 7 and Modeling

The Need for Dimensional Analysis

Dimensional analysis is a process of formulating mechanics problems in terms of nondimensional variables and parameters.

1. Reduction in Variables: F = functional form If F(A1, A2, …, An) = 0, Ai = dimensional variables

Then f(1, 2, … r < n) = 0 j = nondimensional parameters

Thereby reduces number of = j (Ai) experiments and/or simulations i.e., j consists of required to determine f vs. F nondimensional groupings of Ai’s

2. Helps in understanding physics

3. Useful in data analysis and modeling

4. Fundamental to concept of similarity and model testing

Enables scaling for different physical dimensions and fluid properties

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 2 Dimensions and Equations

Basic dimensions: F, L, and t or M, L, and t F and M related by F = Ma = MLT-2

Buckingham  Theorem

In a physical problem including n dimensional variables in which there are m dimensions, the variables can be arranged into r = n – mˆ independent nondimensional parameters r (where usually mˆ = m).

F(A1, A2, …, An) = 0

f(1, 2, … r) = 0

Ai’s = dimensional variables required to formulate problem (i = 1, n)

j’s = nondimensional parameters consisting of groupings of Ai’s (j = 1, r)

F, f represents functional relationships between An’s and r’s, respectively

= rank of dimensional matrix = m (i.e., number of dimensions) usually

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 3 Dimensional Analysis

Methods for determining i’s

1. Functional Relationship Method

Identify functional relationships F(Ai) and f(j)by first determining Ai’s and then evaluating j’s a. Inspection intuition b. Step-by-step Method text c. Exponent Method class

2. Nondimensionalize governing differential equations and initial and boundary conditions

Select appropriate quantities for nondimensionalizing the GDE, IC, and BC e.g. for M, L, and t

Put GDE, IC, and BC in nondimensional form

Identify j’s

Exponent Method for Determining j’s

1) determine the n essential quantities 2) select mˆ of the A quantities, with different dimensions, that contain among them the dimensions, and use them as repeating variables together with one of the other A quantities to determine each . 57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 4

For example let A1, A2, and A3 contain M, L, and t (not necessarily in each one, but collectively); then the j parameters are formed as follows:

x y z Determine exponents   A 1 A 1 A 1 A 1 1 2 3 4 such that i’s are

x2 y2 z2 dimensionless  2  A1 A2 A3 A5

xnm ynm znm 3 equations and 3  nm  A1 A2 A3 An unknowns for each i

In these equations the exponents are determined so that each  is dimensionless. This is accomplished by substituting the dimensions for each of the Ai in the equations and equating the sum of the exponents of M, L, and t each to zero. This produces three equations in three unknowns (x, y, t) for each  parameter.

In using the above method, the designation of mˆ = m as the number of basic dimensions needed to express the n variables dimensionally is not always correct. The correct value for mˆ is the rank of the dimensional matrix, i.e., the next smaller square subgroup with a nonzero determinant.

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 5

Dimensional matrix = A1 ……… An M a11 ……… a1n L aij = exponent t a31 ……… a3n of M, L, or t in o ……… o Ai : : : : : : o ……… o

n x n matrix

Rank of dimensional matrix equals size of next smaller sub-group with nonzero determinant

Example: Hydraulic jump (see section 15.2)

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 6

Say we assume that

V1 = V1(, g, , y1, y2) or V2 = V1y1/y2

Dimensional analysis is a procedure whereby the functional relationship can be expressed in terms of r nondimensional parameters in which r < n = number of variables. Such a reduction is significant since in an experimental or numerical investigation a reduced number of experiments or calculations is extremely beneficial

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 7

1) , g fixed; vary  Represents 2) ,  fixed; vary g many, many 3) , g fixed; vary  experiments

In general: F(A1, A2, …, An) = 0 dimensional form

f(1, 2, … r) = 0 nondimensional form with reduced

or 1 = 1 (2, …, r) # of variables

It can be shown that

V1  y2  Fr   Fr   gy 1  y1  neglect  ( drops out as will be shown) thus only need one experiment to determine the functional relationship

2 1 2 Fr  x  x  x Fr 2 0 0 1/ 2 1  ½ .61 Fr   x1 x 2  1 1 2 1.7 5 3.9

For this particular application we can determine the functional relationship through the use of a control volume analysis: (neglecting  and bottom friction) x-momentum equation: Fx  VxVA 57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 8 y2 y2  1   2  V  V y  V V y  Note: each term 2 2 1 1 1 2 2 2 in equation must have some units:  2 2  2 2 y1  y2  V2 y2  V1 y1  principle of 2 g dimensional homogeneity, i.e., in this case, continuity equation: V1y1 = V2y2 per unit width N/m

V1y1 V2  y2

2 y2   y     y  1 1  2    V2 y  1 1 2  y  1 g 1 y    1    2  = inertial forces due to gravity  y  1 2 y3  y  1 now divide equation by  1  gy 2 2 V1 1 y2  y2   1  dimensionless equation gy 1 2 y1  y1  ratio of inertia forces/gravity forces = ()2 note: Fr = Fr(y2/y1) do not need to know both y2 and y1, only ratio to get Fr Also, shows in an experiment it is not necessary to vary

, y1, y2, V1, and V2, but only Fr and y2/y1 57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 9

Next, can get an estimate of hL from the energy equation (along free surface from 12)

V2 V2 1  y  2  y  h 2g 1 2g 2 L

3 y2  y1  h L  4y1y2

 f() due to assumptions made in deriving 1-D steady flow energy equations

Exponent method to determine j’s for Hydraulic jump

F(g,V1,y1,y2,,) = 0 n = 6 use V1, y1,  as L L M M L L 2 T 3 LT repeating variables T L Assume mˆ = m to avoid evaluating x1 y1 z1 m = 3  r = n – m = 3 rank of 6 x 6 1 = V1 y1   dimensional matrix = (LT-1)x1 (L)y1 (ML-3)z1 ML-1T-1

L x1 + y1  3z1  1 = 0 y1 = 3z1 + 1  x1 = -1 T -x1  1 = 0 x1 = -1 M z1 + 1 = 0 z1 = -1

 1 y1V1 1  or 1  = = Re y1V1 

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 10 x2 y2 z2 2 = V1 y1  g = (LT-1)x2 (L)y2 (ML-3)z2 LT-2

L x2 + y2  3z2 + 1 = 0 y2 =  1  x2 = 1 T -x2  2 = 0 x2 = -2 M z2 = 0 gy V   V 2 y g  1  1/ 2  1 2 1 1 2 2 = Froude number = Fr V1 gy1

x3 y3 z3 3 = V1 y1  y2 = (LT-1)x3 (L)y3 (ML-3)z3 L

L x3 + y3  3z3 + 1 = 0 y3 =  1 T -x3 = 0 M -3z3 = 0 y2 1 y1 3  3  = depth ratio y1 y2 f(1, 2, 3) = 0 or, 2 = 2(1, 3) i.e., Fr = Fr(Re, y2/y1) if we neglect  then Re drops out

V1  y2  Fr   f   gy 1  y1 

Note that dimensional analysis does not provide the actual functional relationship. Recall that previously we used control volume analysis to derive

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 11 2 V1 1 y2  y2   1  gy 1 2 y1  y1  the actual relationship between F vs. y2/y1

F = F(Re, Fr, y1/y2) or Fr = Fr(Re, y1/y2) dimensional matrix:

g V1 y1 y2   M 0 0 0 0 1 1 L 1 1 1 1 3 -1 Size of next smaller t -2 -1 0 0 0 -1 subgroup with nonzero 0 0 0 0 0 0 determinant = 3 = rank 0 0 0 0 0 0 of matrix 0 0 0 0 0 0 57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 12 Common Dimensionless Parameters for Fluid Flow Problems Most common physical quantities of importance in fluid flow problems are: (without heat transfer) 1 2 3 4 5 6 7 8 V, , g, , , K, p, L gravity surface compressibility pressure length tension change

n = 8 m = 3  5 dimensionless parameters

⁄ VL inertia forces V2 / L 1) Reynolds number =  2 Re

 viscous forces V / L

⁄ Rcrit distinguishes among flow regions: laminar or turbulent value varies depending upon flow situation

V inertia forces V2 / L 2) Froude number =  Fr gL gravity force 

important parameter in free-surface flows

V2L inertia force V2 / L 3) =  We  surface tension force  / L2

important parameter at gas-liquid or liquid-liquid interfaces ⁄ and when these surfaces are in contact with a boundary

V V inertia force 4) =   Ma k / a compressibility force

of sound in liquid ⁄ Paramount importance in high speed flow (V > c)

p pressure force p / L 5) Pressure Coefficient =  Cp V2 inertia force V2 / L

(Euler Number) ⁄ 57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 13 Nondimensionalization of the Basic Equation

It is very useful and instructive to nondimensionalize the basic equations and boundary conditions. Consider the situation for  and  constant and for flow with a free surface

Continuity: V  0

DV Momentum:   p  z 2 V Dt g = specific weight Boundary Conditions: 1) fixed solid surface: V  0 2) inlet or outlet: V = Vo p = po  3) free surface: w  p  p  R 1  R 1  t a x y (z = ) surface tension

All variables are now nondimensionalized in terms of  and

U = reference velocity

L = reference length

V tU V*  t*  U L x p  gz x*  p*  L U2 57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 14 All equations can be put in nondimensional form by making the substitution V  V*U

  t* U    t t* t L t*

     ˆi  ˆj kˆ x y z  x*  y*  z*  ˆi  ˆj kˆ x* x y* y z* z 1  * L

u 1  U u* and  Uu*  etc. x L x* L x*

Result: * V*  0 DV*   *p*  *2 V* Dt VL 1) V*  0 Re-1 V p 2) V*  o p*  o U V2 * *  * po gL *  *1 *1 3) w  p   z  R x  R y  t* V2 U2 V2L pressure coefficient -1 Fr-2 We V = U 57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 15 Similarity and Model Testing

Flow conditions for a model test are completely similar if all relevant dimensionless parameters have the same corresponding values for model and prototype

i model = i prototype i = 1, r = n - mˆ (m)

Enables extrapolation from model to full scale

However, complete similarity usually not possible

Therefore, often it is necessary to use Re, or Fr, or Ma scaling, i.e., select most important  and accommodate others as best possible

Types of Similarity:

1) Geometric Similarity (similar length scales): A model and prototype are geometrically similar if and only if all body dimensions in all three coordinates have the same linear-scale ratios

 = Lm/Lp ( < 1)

1/10 or 1/50 2) (similar length and time scales): The motions of two systems are kinematically similar if homologous (same relative position) particles lie at homologous points at homologous times

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 16 3) Dynamic Similarity (similar length, time and force (or mass) scales): in addition to the requirements for kinematic similarity the model and prototype forces must be in a constant ratio

Model Testing in Water (with a free surface)

F(D, L, V, g, , ) = 0

 n = 6 and m = 3 thus r = n – m = 3 pi terms

In a dimensionless form,

f(CD, Fr, Re) = 0 or CD = f(Fr, Re) where

Vm Vp If Frm  Frp or  gL m gL p

Vm  Vp Froude scaling

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 17

VmLm VpLp and Rem = Rep or  m p  VL m m m  3/ 2

 pVL p p Then,

or

However, impossible to achieve, since 8 2 7 2 if  1 10 ,  m 3.1  10m s  1.2  10 m s 72 For mercury  1.2 10 ms

Alternatively one could maintain Re similarity and obtain

Vm = Vp/

But, if , VVmp10 ,

High speed testing is difficult and expensive.

2 V2 V m  p gmLm gpLp

2 gm Vm Lp  2 gp Vp Lm

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 18 2 gm Vm Lp  2 gp Vp Lm

g 1 1 m 3  2    gp  

gp gm  3

But if  1 10 , ggmp1000 Impossible to achieve

Model Testing in Air

F(D, L, V, , , a) = 0

 n = 6 and m = 3 thus r = n – m = 3 pi terms

In a dimensionless form,

f(CD, Re, Ma) = 0 or CD = f(Re, Ma) where

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 19 V L V L If m m  p p m p

V V and m  p a m a p

Then,

or

1  L a  However, m  m  m    p Lp  a p  again not possible

Therefore, in testing Re scaling is also violated

57:020 Mechanics of Fluids and Transport Processes Chapter 7 Professor Fred Stern Fall 2013 20 Model Studies w/o free surface 1 c  p V2 p 2 See High Re text Model Studies with free surface

In hydraulics model studies, Fr scaling used, but lack of We similarity can cause problems. Therefore, often models are distorted, i.e. vertical scale is increased by 10 or more compared to horizontal scale

Ship model testing:

CT = f(Re, Fr) = Cw(Fr) + Cv(Re)

Cwm = CTm  Cv Vm determined Based on flat plate of for Fr scaling same surface area CTs = Cwm + Cv